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Description

  1.  Algebraic description of block codes
  2.  B. Description of a company
  3.  B. Description of a company
  4.  B. Description of a company
  5.  Description
  6.  Description
  7.  Description

The GPWC receives inputs from these units:

- Radio altimeter transceivers

- GPWS module

- Program switch module

- Left and right ADIRUs

- DEU 1 and 2.

The GPWC uses this data to calculate mode 6 alerts:

- Radio altitude

- Landing gear position

- Program pin selection

- Roll attitude

- Decision height.

GPWS - MODE 6 DESCRIPTIONMode 6 is armed when the airplane climbs through 1000 feet

radio altitude. To reset mode 6, the airplane must climb above

the radio altitude where the first altitude callout occurs.

MODE 7 DESCRIPTION




 MODE 1 DESCRIPTION |  General |  Description |  Description |  General |  Description |  General |  Description |  General |  General |

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